Add to ORKGThe model was a full-scale mockup of a light single-engine high-wing monoplane. Tests were made over an angle-of-attack range of -4 deg to 24 deg and over a sideslip range of plus or minus 8 deg at thrust coefficients of 0, 0.14, and 0.30. Control effectiveness and hinge moments were taken on the aileron, elevator, and rudder for a full range of deflections. Downwash measurements at the tail were obtained for the range of thrust coefficient and flap deflection
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
Tests in the Ames 40- by 80-foot wind tunnel of the static longitudinal characteristics of the Repub...
Aerodynamic characteristics of full scale airplane wing model employing sailwing concept and having ...
Full scale wind tunnel investigation of static longitudinal and lateral stability and control charac...
Wind tunnel investigation of static longitudinal and lateral characteristics of full scale mockup of...
Full scale wind tunnel investigation of lateral and longitudinal stability and control characteristi...
Static force data obtained at the NASA Ames Research Center 12 foot Pressure Tunnel are presented in...
Tests were performed in the Langley Unitary Plan wind tunnel to determine the drag and static longit...
The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail ...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Tests were made in the Langley 7- by 10-foot tunnel to determine the lateral-stability characteristi...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Wind tunnel tests of a full-scale model of a light twin engine aircraft were conducted. The angle of...
Full scale wind tunnel tests of low wing, single engine, light aircraft with positive and negative p...
Wind tunnel tests of the 0.16-scale Douglas MX-656 model were made at low and high subsonic Mach num...
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
Tests in the Ames 40- by 80-foot wind tunnel of the static longitudinal characteristics of the Repub...
Aerodynamic characteristics of full scale airplane wing model employing sailwing concept and having ...
Full scale wind tunnel investigation of static longitudinal and lateral stability and control charac...
Wind tunnel investigation of static longitudinal and lateral characteristics of full scale mockup of...
Full scale wind tunnel investigation of lateral and longitudinal stability and control characteristi...
Static force data obtained at the NASA Ames Research Center 12 foot Pressure Tunnel are presented in...
Tests were performed in the Langley Unitary Plan wind tunnel to determine the drag and static longit...
The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail ...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Tests were made in the Langley 7- by 10-foot tunnel to determine the lateral-stability characteristi...
The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...
Wind tunnel tests of a full-scale model of a light twin engine aircraft were conducted. The angle of...
Full scale wind tunnel tests of low wing, single engine, light aircraft with positive and negative p...
Wind tunnel tests of the 0.16-scale Douglas MX-656 model were made at low and high subsonic Mach num...
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
Tests in the Ames 40- by 80-foot wind tunnel of the static longitudinal characteristics of the Repub...
Aerodynamic characteristics of full scale airplane wing model employing sailwing concept and having ...